Accession Number : ADA956526
Title : Experimental Study of Multi-Component Coaxial-Flow Jets in Short Chambers.
Descriptive Note : Contractor rept.,
Corporate Author : UNITED AIRCRAFT RESEARCH LABS EAST HARTFORD CT
Personal Author(s) : Johnson, Bruce V.
Report Date : OCT 1968
Pagination or Media Count : 88
Abstract : Fluid mechanics experiments were performed to obtain information applicable to an open-cycle, coaxial-flow, gaseous nuclear rocket engine. In this engine concept, gaseous nuclear fuel and a surrounding stream of seeded hydrogen propellant pass coaxially through a reactor chamber. The flow was simulated in the present experiments by multi-component, constant-temperature, coaxial-flow jets in short chambers. The flow was studied using flow visualization techniques and concentration measurements.
Descriptors : *ROCKET ENGINES, *FLUID MECHANICS, EXPERIMENTAL DATA, DATA ACQUISITION, FLOW VISUALIZATION, CHAMBERS.
Subject Categories : Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE